Kawasaki Ki-10

Kawasaki Ki-10

The Kawasaki Ki-10, designated as the Army Type 95 Fighter,

was the last biplane fighter adopted by the Imperial Japanese Army Air Force (IJAAF).

Designed by Takeo Doi and introduced in 1935, it was chosen over the more modern monoplane Nakajima Ki-11 due to its superior manoeuvrability—a trait highly valued in Japanese aerial doctrine at the time.

Design and Capabilities

Engine

Kawasaki Ha-9-IIb

liquid-cooled V12,

850 hp 

Armament

Two synchronized 7.7 mm Type 89 machine guns 

Max Speed

~400 km/h 

Range

~1,100 km 

Service Ceiling

~11,500 m 

Construction

All-metal frame with fabric-covered surfaces; unequal-span biplane wings with upper ailerons

Early Combat Use

The Ki-10 saw its first combat during the Second Sino-Japanese War, beginning in 1937:

Deployed in Manchukuo and North China, it escorted bombers and engaged Chinese fighters such as the Curtiss Hawk II and Vought V-65C Corsair.

One notable engagement occurred over Taiyuan, where Ki-10s clashed with Chinese aircraft.

Although they scored some victories, Japanese ace Major Hiroshi Miwa was shot down and killed by Captain Chan Kee-Wong of the Chinese Air Force.

Decline and Obsolescence

By 1939, during the Nomonhan Incident (Battles of Khalkhin Gol against Soviet forces), the Ki-10 was clearly outclassed by newer Soviet monoplanes like the Polikarpov I-16.

It was gradually replaced by the more advanced Nakajima Ki-27.

Secondary Roles in WWII

Although obsolete by the start of the Pacific War, the Ki-10 was retained for:

Training missions

Short-range patrols

Reconnaissance duties in Japan and occupied China (notably in early 1942).

A total of 588 units were built, including prototypes and both production variants

Ki-10-I

300 units 

Ki-10-II

280 units (with improved stability and longer fuselage)

Legacy

The Ki-10’s service life reflects Japan’s transitional phase from biplane to monoplane fighters.

Though outdated by WWII standards, it played a formative role in shaping IJAAF tactics and pilot training in the late 1930s.

The Variants

Ki-10 (Prototype)

Built

4 units (early 1935)

Purpose

Evaluation aircraft for IJAAF trials

Notes

These prototypes were constructed to compete against Nakajima’s Ki-11 monoplane.

Despite the Ki-11’s superior speed, the Ki-10 prototypes demonstrated a better climb rate and turning ability—qualities the IJAAF prioritised.

Outcome

Selected for production as the Army Type 95 Fighter.

Ki-10-I

(Army Fighter Type 95-I)

Built

300 units (Dec 1935 – Oct 1937)

Role

First production model; frontline fighter during the early Second Sino-Japanese War

Features

All-metal frame with fabric-covered wings

Kawasaki Ha-9-IIa V12 engine (~850 hp)

Two synchronized 7.7 mm Type 89 machine guns

Combat Use

Deployed in China for bomber escort and air superiority missions.

Engaged Chinese aircraft, like the Curtiss Hawk II and Vought Corsair.

Its agility made it effective in early dogfights, though it lacked armour and modern speed.

Ki-10-II (Prototype)

Built

1 unit (May 1936)

Purpose

Experimental upgrade of Ki-10-I

Modifications

Lengthened fuselage for improved longitudinal stability

Slightly increased wingspan

Outcome

Served as the basis for the improved Ki-10-II production model.

Ki-10-II

(Army Fighter Type 95–2)

Built

280 units (June 1937 – Dec 1938)

Role

Enhanced production variant

Improvements

Better stability and control at high speeds

Refined aerodynamics and strengthened airframe

Operational Use

Continued service in China and Manchuria; some units participated in the Nomonhan Incident (1939) against Soviet forces, where they were outclassed by Polikarpov I-16 monoplanes.

Ki-10-I KAI

Built

1 unit (Oct 1936)

Purpose

Engine and radiator testbed

Modifications

Revised cooling system

Minor aerodynamic tweaks

Outcome

Used to evaluate performance enhancements for future variants.

Ki-10-II KAI

Built

2 units (Nov 1937)

Purpose

Advanced aerodynamic prototype

Features

Streamlined airframe

Powered by the Kawasaki Ha-9-IIb engine (850 hp)

Designation Confusion

Despite being based on the Ki-10-II, it was re-designated as Ki-10-I KAI due to its experimental nature.

Outcome

Did not enter production but informed later monoplane designs.

Specifications

Crew

1

Length

7.2 m (23 ft 7 in)

Wingspan

10.02 m (32 ft 10 in)

Height

3 m (9 ft 10 in)

Wing area

23 m² (250 sq ft)

Airfoil

NACA M-12

Empty weight

1,360 kg (2,998 lbs)

Gross weight

1,740 kg (3,836 lbs)

Powerplant

1 × Kawasaki Ha9-IIa V-12,

liquid-cooled piston engine,

634 kW (850 hp)

Propellers

3-bladed fixed-pitch metal propeller

Performance

Maximum speed

400 km/h (250 mph, 220 kn) at 3,000 m (9,800 ft)

Service ceiling

11,500 m (37,700 ft)

Rate of climb

16.67 m/s (3,300 ft/min)

Wing loading

75.7 kg/m² (15.5 lbs/sq ft)

Power/mass

0.36 kW/kg (0.22 hp/lb)

Armament

2 × fixed, forward-firing 7.7 mm (.303 in)

Type 89 machine guns.

 

 

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